Remote nanosatellite formation designs with orbit perturbation corrections and attitude control/propulsion subsystem correlation
The innovative idea of distributing the functionality of current larger satellites among smaller, cooperative satellites has been sincerely considered for assorted space missions to accomplish goals that are not possible or very difficult to do with a single satellite. Additionally, the utilization...
| Main Author: | |
|---|---|
| Other Authors: | |
| Language: | en_US |
| Published: |
Monterey, California. Naval Postgraduate School
2012
|
| Online Access: | http://hdl.handle.net/10945/7781 |